Aerospace Instrument-Making Annotation << Back Simulation of load application process to elastic inertial object in the test bed A.I. Belousov, G.I. Rastorguev, O.R. Fedotova This paper presents the problem of modeling process application load on the fixed elastic wing of aircraft. Loading aircraft wing is carried out by use hydraulic cylinders of bilateral action and rigid lever system. At modeling takes into account inertial properties both the plane and lever system. On models are investigated parameters of the systems stand on stability of process loading. Models are realized for single-channel and four-channel loading of aircraft wing. Possible laws of management the appendix of loads are analyzed. Key words: modeling; aircraft; test; loading; control. E-mail: fedotova@craft.nstu.ru